A study of Z-crimp structural parameters impact on strength under transverse compression and longitudinal shear
Russian aeronautics ; 56 , 1
2013
Article (Journal)
English
BKL: | 55.50 Luftfahrzeugtechnik | |
Local classification TIB: | 770/7040/8000 |
Ultimate strength of stiffened plates with a transverse crack under uniaxial compression
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